NTSB CAROL · Event
Event CHI03FA239
Registry · N1068S
FAA Aircraft Registry record.
Make / Model
ANGLIN SPECIAL AERO PLANES INC J-3 KITTEN
Year of manufacture
1984 · 19 years old at event
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20071215
ADS-B equipped
Yes — Mode-S A01E7F
Registrant of record
ANDREZEJ SITARZ
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to abort the takeoff, his improper use of flaps during the takeoff, and his failure to attain sufficient airspeed resulting in an inadvertent stall and subsequent impact with a road.
Factual narrative
On August 2, 2003, about 0920 central daylight time, an amateur-built Gerlach Skyraider II, N1068S, piloted by a private pilot, sustained substantial damage when it impacted a road after takeoff from the northwest ultralight runway (1,200 feet by 100 feet, turf), at the Wittman Regional Airport, Oshkosh, Wisconsin. The flight was performed during the annual Experimental Aircraft Association gathering. The pilot reported that the engine lost power during the takeoff. The 14 CFR Part 91 business flight was operating in visual meteorological conditions without a flight plan. The pilot and passenger were not injured. The local flight was originating when the accident occurred. In a written report of the accident, the pilot stated that the takeoff roll was long and the airplane's engine seemed to lose power. He stated that he "released [the] flaps to gain speed but the engine seem[ed] to have less power." The pilot said that after clearing the fence at the end of the runway, he turned right and crashed on the road. In his written report, the pilot listed no mechanical malfunction of the airplane. In a written statement to the Winnebago County Sheriff's Department, the pilot stated that the engine power "wasn't up to its normal standard. It did takeoff [and] seemed to get better but all of a sudden it seemed to lose power again. I tried to release the flaps to get some speed and the plane didn't respond." The pilot stated that the airplane kept losing speed and power. He stated that when the airplane cleared the fence, he attempted to land on the road. The passenger reported that the accident flight was his second flight of the day in the accident airplane. He stated that on the accident flight the pilot used flaps during the takeoff. He stated that, in his opinion, the use of the flaps produced enough drag to slow the aircraft's speed on takeoff. A witness stated that he observed the accident airplane during the takeoff. He stated that the airplane was "going too slow, too low, and it was climbing too steeply." The witness stated that the airplane then stalled and struck the ground. He stated that the airplane's engine was running until the airplane struck the ground. A postaccident examination of the airplane revealed no pre-impact anomalies. The airplane was substantially damaged when it impacted a road after takeoff. The pilot reported that the takeoff roll was long and the airplane's engine seemed to lose power. He stated that he "released [the] flaps to gain speed but the engine seem[ed] to have less power." The pilot said that after clearing the fence at the end of the runway, he turned right and crashed on the road. The passenger reported that on the accident flight the pilot used flaps during the takeoff and, in his opinion, the use of the flaps produced enough drag to slow the aircraft's speed on takeoff. A witness stated that he observed the accident airplane during the takeoff, and the airplane was "going too slow, too low, and was climbing too steeply." The witness stated that the airplane then stalled and struck the ground. He stated that the airplane's engine was running until the airplane struck the ground. In his written report, the pilot listed no mechanical malfunction of the airplane. A postaccident examination of the airplane revealed no pre-impact anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_CHI03FA239.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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